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59315 (1999 CC89)
Classification: Main-belt Asteroid          SPK-ID: 2059315
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1969764544201806 4.0133e-08  
a 2.43215250740316 1.0501e-08 au
q 1.953075729885733 9.4144e-08 au
i 3.102058694367556 5.6657e-06 deg
node 117.0159657483098 8.4948e-05 deg
peri 318.9146772158974 8.6465e-05 deg
M 162.7259091193832 1.6552e-05 deg
tp 2457974.262834461179
(2017-Aug-08.76283446)
6.1965e-05 TDB
period 1385.430143325108
3.79
8.9725e-06
2.457e-08
d
yr
n .2598470963941785 1.6829e-09 deg/d
Q 2.911229284920586 1.2569e-08 au
  Orbit Determination Parameters
   # obs. used (total)      732  
   data-arc span      8081 days (22.12 yr)  
   first obs. used      1996-05-18  
   last obs. used      2018-07-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51601  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Oct-04 01:31:20  

Additional Information
 Earth MOID = .969454 au 
 Jupiter MOID = 2.35404 au 
 T_jup = 3.478 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.6   n/a MPO436196  
diameter diameter 1.718 km 0.455 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.261   0.072 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

59315 (1999 CC89)          Discovered 1999-Feb-10 by LINEAR at Socorro
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1999 CC89 = 2001 RA100 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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